US4348905A - Vibration sensor for an automotive vehicle - Google Patents
Vibration sensor for an automotive vehicle Download PDFInfo
- Publication number
- US4348905A US4348905A US06/166,947 US16694780A US4348905A US 4348905 A US4348905 A US 4348905A US 16694780 A US16694780 A US 16694780A US 4348905 A US4348905 A US 4348905A
- Authority
- US
- United States
- Prior art keywords
- vibrator
- vibration
- housing
- vibration sensor
- cavity
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000000463 material Substances 0.000 claims description 14
- 230000008646 thermal stress Effects 0.000 abstract description 3
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000012212 insulator Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000010137 moulding (plastic) Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B06—GENERATING OR TRANSMITTING MECHANICAL VIBRATIONS IN GENERAL
- B06B—METHODS OR APPARATUS FOR GENERATING OR TRANSMITTING MECHANICAL VIBRATIONS OF INFRASONIC, SONIC, OR ULTRASONIC FREQUENCY, e.g. FOR PERFORMING MECHANICAL WORK IN GENERAL
- B06B1/00—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency
- B06B1/02—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency making use of electrical energy
- B06B1/06—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency making use of electrical energy operating with piezoelectric effect or with electrostriction
- B06B1/0603—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency making use of electrical energy operating with piezoelectric effect or with electrostriction using a piezoelectric bender, e.g. bimorph
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01H—MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
- G01H11/00—Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves by detecting changes in electric or magnetic properties
- G01H11/06—Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves by detecting changes in electric or magnetic properties by electric means
- G01H11/08—Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves by detecting changes in electric or magnetic properties by electric means using piezoelectric devices
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L23/00—Devices or apparatus for measuring or indicating or recording rapid changes, such as oscillations, in the pressure of steam, gas, or liquid; Indicators for determining work or energy of steam, internal-combustion, or other fluid-pressure engines from the condition of the working fluid
- G01L23/22—Devices or apparatus for measuring or indicating or recording rapid changes, such as oscillations, in the pressure of steam, gas, or liquid; Indicators for determining work or energy of steam, internal-combustion, or other fluid-pressure engines from the condition of the working fluid for detecting or indicating knocks in internal-combustion engines; Units comprising pressure-sensitive members combined with ignitors for firing internal-combustion engines
- G01L23/221—Devices or apparatus for measuring or indicating or recording rapid changes, such as oscillations, in the pressure of steam, gas, or liquid; Indicators for determining work or energy of steam, internal-combustion, or other fluid-pressure engines from the condition of the working fluid for detecting or indicating knocks in internal-combustion engines; Units comprising pressure-sensitive members combined with ignitors for firing internal-combustion engines for detecting or indicating knocks in internal combustion engines
- G01L23/222—Devices or apparatus for measuring or indicating or recording rapid changes, such as oscillations, in the pressure of steam, gas, or liquid; Indicators for determining work or energy of steam, internal-combustion, or other fluid-pressure engines from the condition of the working fluid for detecting or indicating knocks in internal-combustion engines; Units comprising pressure-sensitive members combined with ignitors for firing internal-combustion engines for detecting or indicating knocks in internal combustion engines using piezoelectric devices
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/08—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
- G01P15/09—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by piezoelectric pick-up
- G01P15/0922—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by piezoelectric pick-up of the bending or flexing mode type
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04R—LOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKE ACOUSTIC ELECTROMECHANICAL TRANSDUCERS; DEAF-AID SETS; PUBLIC ADDRESS SYSTEMS
- H04R17/00—Piezoelectric transducers; Electrostrictive transducers
- H04R17/10—Resonant transducers, i.e. adapted to produce maximum output at a predetermined frequency
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/02—Indexing codes associated with the analysed material
- G01N2291/028—Material parameters
- G01N2291/02827—Elastic parameters, strength or force
Definitions
- the present invention relates generally to a vibration sensor for an automotive vehicle which can detect mechanical vibrations generated from an internal combustion engine, such as knocking, and more specifically to a vibration sensor for an automotive vehicle having a piezoelectric vibration element therein mounted in cantilever fashion.
- a vibration sensor is indispensable in order to detect the knocking conditions of an internal combustion engine, that is, to detect the engine vibration accompanied with knocking.
- a round-shape piezoelectric vibration element has been used for this vibration sensor. Since a conventional round-shape piezoelectric vibration is fixed to the housing at its periphery, the vibration is susceptible to thermal deformation whenever the temperature changes sharply, thereby resulting in a change in resonant frequency of the vibrator.
- the vibrator sensor of the present invention comprises a housing with a hollow cavity, a piezoelectric element mounted therein in cantilever fashion, and two lead wires, one end of the vibrator being fixed to the housing, the other end thereof being free to vibrate within the hollow cavity.
- the two lead wires attached to the vibrator to conduct a piezoelectric signal are fixed to the vibrator by a bonding material or in a one-step plastic molding process.
- FIG. 1 is a vertical sectional view of a prior art vibration sensor
- FIG. 2 is a vertical sectional view showing an embodiment of the vibration sensor according to the present invention.
- FIG. 3 is a bottom view of the embodiment shown in FIG. 2;
- FIG. 4 is a vertical sectional view showing another embodiment of the vibration sensor according to the present invention.
- FIG. 5 is a vertical sectional view showing a third embodiment of the vibration sensor according to the present invention.
- FIGS. 6 (A), (B) and (C) are vertical longitudinal sectional views showing piezoelectric vibration elements of various types.
- the numeral 1 denotes a thin, round diaphragm vibrator made of a piezoelectric element, both surfaces of which are coated by, for example, silver to form electrode surfaces.
- the vibrator 1 is housed in a housing 2 having a concave portion 3, and is clamped by an electrode 5 having a flange 6 to form another concave portion 4.
- the vibrator 1 is excited by the housing 2 to produce diaphragm vibration.
- One of the electrode surfaces of the vibrator 1 is connected to the conductive housing 2; the other is connected to the conductive electrode 5.
- a dish-shaped spring 9 is placed between a spring sheet 8 and a retainer 10.
- the numeral 7 denotes an insulator.
- the retainer 10 is fixed by bending inward the cylindrical housing end to form a flange portion 11.
- the diaphragm vibrator 1 Since the diaphragm vibrator 1 is clamped by the elastic force of the dish-shaped spring 9 under almost constant pressure, it is possible to prevent the resonant frequency of the vibrator 1 from being varied according to the vibrator fixing pressure.
- the diameter of the concave portion 3 of the housing 2 is designed to be equal to that of the concave portion 4, so that the vibrator supporting internal diameters of both parts coincide.
- the support internal diameter is determined so that a resonant frequency of the vibrator 1 may range over the usual engine knocking frequencies between 5 and 9 KHZ.
- the vibration sensor thus constructed is fixed onto an engine body with an anchor bolt 12 integrally formed with the housing 2.
- the base portion 13 of the housing 2 is hexagonal in shape for easy grasping with conventional mechanics' tools.
- the vibrator 1 When the vibrator 1 begins to vibrate up and down with its periphery as the fulcrum in tune with the vibration of an engine body, a difference in potential is generated between the two electrode surfaces of the piezoelectric element in accordance with the deformation rate. Since one electrode surface is grounded through the housing 2, it is possible to transduce a mechanical vibration of the vibrator 1 (of the piezoelectric element) into a voltage signal between the electrode 5 and the engine body ground. Further, since the vibrator 1 is so designed to resonate within the knocking frequency range of an engine, it is possible to detect the vibration due to knocking efficiently and accurately.
- the vibrator of this type has the following shortcomings:
- the vibrator Since the vibrator is fixedly supported at its periphery, when the temperature within the vibrator changes sharply, internal stress of tension or contraction within the vibrator results in deformation of the vibrator. That is to say, the vibrator is, therefore, susceptible to changes in resonant frequency.
- FIGS. 2, 3, 4, 5 and 6, and more specifically to FIG. 2, wherein a preferred embodiment of the vibrator sensor of the present invention is illustrated.
- the numeral 20 denotes a housing having a hollow cavity 21 in which a vibrator 22 is mounted and having an anchor bolt 31 integrally formed therewith.
- the vibrator 22 comprises two rectangular, thin piezoelectric elements 23 and 24 adhered to each other with a conductive bonding material, and electrode surfaces coated on both the sides of the piezoelectric element.
- a Bimorph cell the vibrator 22 of this type is constructed so that the electrode surfaces of the same polarity face each other so that piezoelectricity of each element will be doubled when the two elements are bent in the same direction.
- One end of the vibrator 22 is initially inserted into a second cavity 25 after being passed through an elongate opening slit 26.
- Lead wires 28 and 29 are connected to the electrode surfaces of the piezoelectric elements 23 and 24 by, for example, soldering.
- the lead wires 28 and 29 extend from the second cavity 25, as shown.
- the vibrator 22 is next fixed within the second cavity 25 with a bonding material 27 so that the effective length thereof is determined by the distance from the end surface of the slit 26 to the free end of the vibrator.
- protective cover 30 is fitted to the housing 20 from the outside.
- the numeral 32 in FIG. 3 denotes a hexagonal portion of the housing, which is used when mounting the vibration sensor to an engine body.
- the vibrator 22 is excited with the supported end as the fulcrum whenever vibration is transmitted from the engine body to the vibrator housing 20.
- the piezoelectric elements 23 and 24 generate an electric signal to be transmitted through the lead wires 28 and 29.
- the vibrator 22 is first mounted so as to have a relatively low resonant frequency and is next adjusted into a desired length by cutting off the free end of the vibrator 22 so as to have a desired resonant frequency.
- the vibrator 22 mounted in such cantilever fashion is not subject to thermal stress. Therefore the vibrator characteristics are kept stable despite a temperature rise from the engine body.
- the positions where the lead wires 28 and 29 are soldered onto the vibrator electrode surfaces are fully covered by a bonding material, and therefore the lead wires are prevented from being peeled off from the surfaces even if the vibrator vibrates strongly.
- FIG. 4 shows another embodiment of the present invention.
- a housing 20 is integrally molded as one body from a plastic material and one end of the piezoelectric vibrator 22 and two lead wires 28 and 29 are all embedded together into the housing in a one-step process, without the use of any bonding material.
- FIG. 5 shows the third embodiment of the present invention.
- a housing 20 is formed with an additional passageway from the second cavity 25 and the lead wires are taken out therethrough.
- a vibrator 22 is fixed within the hollow cavity 21 by introducing a bonding material into the second cavity 25. In this embodiment, it is possible to regulate the effective length of the vibrator by adjusting the amount of bonding material.
- a metal plate 41 is bonded by a conductive bonding material to one side of a dual electrode piezoelectric element 40; in FIG. 6 (B), the metal plate is bonded by a conductive bonding material between two piezoelectric elements 40; and in FIG. 6 (C), the metal plate is bonded to one side of two piezoelectric elements bonded to each other. In these cases, the metal plate 41 is used for reinforcing the vibrator element.
- the vibrator of the present invention is not subject to deformation due to thermal stress, and therefore is able to accurately detect knocking vibrations of an engine body where temperature changes frequently and sharply.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Signal Processing (AREA)
- Mechanical Engineering (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
- Measuring Fluid Pressure (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP54-96577[U] | 1979-07-13 | ||
JP1979096577U JPS5613719U (zh) | 1979-07-13 | 1979-07-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
US4348905A true US4348905A (en) | 1982-09-14 |
Family
ID=14168822
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US06/166,947 Expired - Lifetime US4348905A (en) | 1979-07-13 | 1980-07-08 | Vibration sensor for an automotive vehicle |
Country Status (5)
Country | Link |
---|---|
US (1) | US4348905A (zh) |
JP (1) | JPS5613719U (zh) |
CA (1) | CA1156345A (zh) |
DE (1) | DE3026394A1 (zh) |
GB (1) | GB2056763B (zh) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4494409A (en) * | 1981-05-29 | 1985-01-22 | Kabushiki Kaisha Toyota Chuo Kenkyusho | Engine vibration sensor |
US4628735A (en) * | 1984-12-14 | 1986-12-16 | Sundstrand Data Control, Inc. | Vibrating beam accelerometer |
US4713573A (en) * | 1984-06-29 | 1987-12-15 | Robert Bosch Gmbh | Trigger mechanism construction for an automotive passenger restraint system |
US5235237A (en) * | 1990-02-14 | 1993-08-10 | Endevco Corporation | Surface-mount piezoceramic accelerometer and method for making |
US6257065B1 (en) | 1999-03-24 | 2001-07-10 | Meritor Heavy Systems, L.L.C. | Strain gauge vibration sensor |
US6479368B1 (en) * | 1998-03-02 | 2002-11-12 | Kabushiki Kaisha Toshiba | Method of manufacturing a semiconductor device having a shallow trench isolating region |
US10895561B2 (en) | 2017-12-15 | 2021-01-19 | Industrial Technology Research Institute | Embedded sensor module and sensing device |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE441127B (sv) * | 1984-01-25 | 1985-09-09 | Asea Ab | Accelerometer |
JPH01174278A (ja) * | 1987-12-28 | 1989-07-10 | Misuzu Erii:Kk | インバータ |
EP0351038A1 (en) * | 1988-06-10 | 1990-01-17 | Hewlett-Packard Company | Improved accelerometer and method of manufacture |
US5539270A (en) * | 1993-11-19 | 1996-07-23 | Matsushita Electric Works, Ltd. | Acceleration detector |
JPH0862242A (ja) * | 1994-07-29 | 1996-03-08 | Whitaker Corp:The | 加速度センサ |
DE19746898A1 (de) * | 1997-10-23 | 1999-05-12 | Siemens Ag | Klopfsensor |
DE10114045A1 (de) * | 2001-03-22 | 2002-10-02 | Bosch Gmbh Robert | Schwingungsaufnehmer zur Befestigung an einem Schwingungen aufweisenden Bauteil |
DE10140678A1 (de) * | 2001-08-24 | 2003-03-13 | Sew Eurodrive Gmbh & Co | Verschlussschraube und eine Baureihe von Verschlussschraube |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2619605A (en) * | 1944-01-10 | 1952-11-25 | Sperry Corp | Vibration or impact indicator |
US3113223A (en) * | 1960-07-27 | 1963-12-03 | Space Technology Lab Inc | Bender-type accelerometer |
US3387149A (en) * | 1965-12-21 | 1968-06-04 | Nasa | Phonocardiograph transducer |
US4103264A (en) * | 1976-01-30 | 1978-07-25 | Vernitron Corporation | Wave filter and process for making same |
-
1979
- 1979-07-13 JP JP1979096577U patent/JPS5613719U/ja active Pending
-
1980
- 1980-06-26 GB GB8020985A patent/GB2056763B/en not_active Expired
- 1980-07-08 US US06/166,947 patent/US4348905A/en not_active Expired - Lifetime
- 1980-07-11 DE DE19803026394 patent/DE3026394A1/de not_active Withdrawn
- 1980-07-11 CA CA000356011A patent/CA1156345A/en not_active Expired
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2619605A (en) * | 1944-01-10 | 1952-11-25 | Sperry Corp | Vibration or impact indicator |
US3113223A (en) * | 1960-07-27 | 1963-12-03 | Space Technology Lab Inc | Bender-type accelerometer |
US3387149A (en) * | 1965-12-21 | 1968-06-04 | Nasa | Phonocardiograph transducer |
US4103264A (en) * | 1976-01-30 | 1978-07-25 | Vernitron Corporation | Wave filter and process for making same |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4494409A (en) * | 1981-05-29 | 1985-01-22 | Kabushiki Kaisha Toyota Chuo Kenkyusho | Engine vibration sensor |
US4713573A (en) * | 1984-06-29 | 1987-12-15 | Robert Bosch Gmbh | Trigger mechanism construction for an automotive passenger restraint system |
US4628735A (en) * | 1984-12-14 | 1986-12-16 | Sundstrand Data Control, Inc. | Vibrating beam accelerometer |
US5235237A (en) * | 1990-02-14 | 1993-08-10 | Endevco Corporation | Surface-mount piezoceramic accelerometer and method for making |
US6479368B1 (en) * | 1998-03-02 | 2002-11-12 | Kabushiki Kaisha Toshiba | Method of manufacturing a semiconductor device having a shallow trench isolating region |
US6257065B1 (en) | 1999-03-24 | 2001-07-10 | Meritor Heavy Systems, L.L.C. | Strain gauge vibration sensor |
US10895561B2 (en) | 2017-12-15 | 2021-01-19 | Industrial Technology Research Institute | Embedded sensor module and sensing device |
Also Published As
Publication number | Publication date |
---|---|
GB2056763B (en) | 1984-01-18 |
DE3026394A1 (de) | 1981-01-29 |
CA1156345A (en) | 1983-11-01 |
JPS5613719U (zh) | 1981-02-05 |
GB2056763A (en) | 1981-03-18 |
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Legal Events
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STCF | Information on status: patent grant |
Free format text: PATENTED CASE |